- Jun 8, 2020
I hope you know that GTRE had many ISRO help in its initial phase when kaveri engine was not on even in drawing phaseRocket engines are fundamentally different from gas turbines. Although a turbopump is used in liquid fuelled engines, it's combustion temperature is only around 850-1000K. Air-breathing turbines reach far higher temperatures. This is why ISRO scientists and engineers are not suitable for this job.
Again my pov is no foreign help
Like we made one of the powerful second stage thruster for our cryogenic by our indigenious way
This too can be made